View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 66441U 26145.46085103 +.00000000 +00000-0 +51933-3 0 00003
2 66441 43.0029 200.6753 0001742 271.7147 88.3505 15.27589004 07
| Epoch (UTC): | 25 May 2026 11:03:37 |
| Eccentricity: | 0.0001742 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.6753° |
| argument of perigee: | 271.7147° |
| revolutions per day: | 15.27589004 |
| mean anomaly at epoch: | 88.3505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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